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Miniature, unmanned aircraft with onboard stabilization and automated ground control of flight path

机译:微型无人飞机,具有机载稳定功能和飞行路径的自动地面控制

摘要

A miniature, unmanned aircraft for acquiring and/or transmitting data, capable of automatically maintaining desired airframe stability while operating by remote directional commands. The aircraft comprises a fuselage and a wing, a piston engine and propeller, a fuel supply, at least one data sensor and/or radio transceiver, a microprocessor disposed to manage flight, a radio transceiver for receiving remotely generated flight direction commands, a GPS receiver, a plurality of control surfaces and associated servomechanisms, for controlling flight stabilization and direction, roll, pitch, yaw, velocity, and altitude sensors. The microprocessor uses roll, pitch, yaw, and altitude data to control attitude and altitude of the aircraft automatically, but controls flight direction solely based on external commands. The aircraft does not exceed fifty-five pounds.
机译:一种用于获取和/或发送数据的微型无人飞机,能够在通过远程定向命令进行操作时自动保持所需的机身稳定性。该飞机包括机身和机翼,活塞发动机和螺旋桨,燃料供应,至少一个数据传感器和/或无线电收发器,布​​置为管理飞行的微处理器,用于接收远程生成的飞行方向命令的无线电收发器,GPS接收器,多个控制表面和相关的伺服机构,用于控制飞行稳定度和方向,侧倾,俯仰,偏航,速度和高度传感器。微处理器使用侧倾,俯仰,偏航和高度数据自动控制飞机的姿态和高度,但仅根据外部命令控制飞行方向。飞机不超过五十五磅。

著录项

  • 公开/公告号US6847865B2

    专利类型

  • 公开/公告日2005-01-25

    原文格式PDF

  • 申请/专利权人 ERNEST A. CARROLL;

    申请/专利号US20020255183

  • 发明设计人 ERNEST A. CARROLL;

    申请日2002-09-26

  • 分类号B64C1320;

  • 国家 US

  • 入库时间 2022-08-21 22:19:41

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